EP2038536A4 - Moteur à méthane pour propulsion de fusée - Google Patents

Moteur à méthane pour propulsion de fusée

Info

Publication number
EP2038536A4
EP2038536A4 EP07715521A EP07715521A EP2038536A4 EP 2038536 A4 EP2038536 A4 EP 2038536A4 EP 07715521 A EP07715521 A EP 07715521A EP 07715521 A EP07715521 A EP 07715521A EP 2038536 A4 EP2038536 A4 EP 2038536A4
Authority
EP
European Patent Office
Prior art keywords
rocket propulsion
methane engine
methane
engine
rocket
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP07715521A
Other languages
German (de)
English (en)
Other versions
EP2038536A1 (fr
Inventor
Kyoung Ho Kim
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
C and Space Inc
Original Assignee
C and Space Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by C and Space Inc filed Critical C and Space Inc
Publication of EP2038536A1 publication Critical patent/EP2038536A1/fr
Publication of EP2038536A4 publication Critical patent/EP2038536A4/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/425—Propellants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/46—Feeding propellants using pumps
    • F02K9/48—Feeding propellants using pumps driven by a gas turbine fed by propellant combustion gases or fed by vaporized propellants or other gases
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/56—Control
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/56—Control
    • F02K9/58—Propellant feed valves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • F02K9/64—Combustion or thrust chambers having cooling arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Toys (AREA)
EP07715521A 2006-07-07 2007-03-07 Moteur à méthane pour propulsion de fusée Withdrawn EP2038536A4 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
KR1020060064106A KR100674118B1 (ko) 2006-07-07 2006-07-07 로켓 추진용 메탄엔진
PCT/KR2007/001121 WO2008004744A1 (fr) 2006-07-07 2007-03-07 Moteur à méthane pour propulsion de fusée

Publications (2)

Publication Number Publication Date
EP2038536A1 EP2038536A1 (fr) 2009-03-25
EP2038536A4 true EP2038536A4 (fr) 2011-05-11

Family

ID=38014820

Family Applications (1)

Application Number Title Priority Date Filing Date
EP07715521A Withdrawn EP2038536A4 (fr) 2006-07-07 2007-03-07 Moteur à méthane pour propulsion de fusée

Country Status (5)

Country Link
US (1) US20090013663A1 (fr)
EP (1) EP2038536A4 (fr)
JP (1) JP4824814B2 (fr)
KR (1) KR100674118B1 (fr)
WO (1) WO2008004744A1 (fr)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100925858B1 (ko) 2008-08-22 2009-11-06 (주)씨앤스페이스 로켓 추진용 메탄엔진의 터보펌프
US20110179766A1 (en) * 2009-10-27 2011-07-28 Fly Steam, LLC Heat recovery system
KR101310736B1 (ko) 2012-06-04 2013-09-25 한국항공우주연구원 다단 연소사이클 액체메탄 로켓엔진 시스템
FR2997731B1 (fr) 2012-11-06 2018-07-27 Arianegroup Sas Dispositif et procede d'alimentation d'un moteur-fusee
FR3006380B1 (fr) * 2013-05-31 2017-05-19 Pierre Francois Yannick Agostini Dispositif de propulsion hybride de type "aerobie et anaerobie" a fonctionnement en regime permanent de type combine et simultane et systeme et ensembles propulses comportant un tel dispositif
EP3199792B1 (fr) 2014-09-25 2021-02-24 Patched Conics, LLC Dispositif et procédé pour mettre sous pression et alimenter un fluide
US10605204B2 (en) 2017-03-09 2020-03-31 The Government Of The United States Of America, As Represented By The Secretary Of The Navy Methane/oxygen rocket engine with specific impulse enhancement by hot helium infusion
US10718294B1 (en) * 2017-10-27 2020-07-21 United Launch Alliance, L.L.C. Integrated vehicle fluids
KR102169985B1 (ko) * 2019-08-19 2020-10-26 한국항공우주연구원 로켓 엔진의 재점화를 위한 점화 시스템
CN111664024A (zh) * 2020-07-07 2020-09-15 西安空天引擎科技有限公司 一种过氧化氢煤油自增压动力系统
KR102469946B1 (ko) * 2020-12-31 2022-11-23 한국항공우주연구원 연소기 헤드-터보펌프 일체형 로켓엔진
CN113154391B (zh) * 2021-04-27 2023-08-04 西安航天动力研究所 一种气氧气甲烷火炬点火装置及其火炬生成方法
CN113090413B (zh) * 2021-05-12 2025-11-25 星际荣耀航天科技集团股份有限公司 开式变推力火箭发动机、火箭及控制方法
CN114645803B (zh) * 2022-03-17 2024-06-25 北京航空航天大学 一种复合材料缠绕再生冷却推力室及加工工艺
KR102793784B1 (ko) * 2022-08-04 2025-04-11 한국항공우주연구원 로켓추진기관
CN117823297A (zh) * 2023-03-27 2024-04-05 海南太空科技有限公司 一种液体火箭点火方法
WO2025239563A1 (fr) * 2024-05-14 2025-11-20 우나스텔라 주식회사 Moteur-fusée à ergols liquides à cycle de pompe électrique doté d'un système de dérivation de comburant à des fins de refroidissement, de mise sous pression et d'allumage
CN119000994B (zh) * 2024-10-21 2025-03-14 北京自动化控制设备研究所 一种高速热气流发生装置、方法及受感器烧蚀试验系统

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3267664A (en) * 1963-03-19 1966-08-23 North American Aviation Inc Method of and device for cooling
US4831818A (en) * 1988-03-09 1989-05-23 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Dual-fuel, dual-mode rocket engine
US4879874A (en) * 1986-05-07 1989-11-14 National Space Development Agency Of Japan Liquid fuel rocket engine
US6619031B1 (en) * 2000-04-27 2003-09-16 Vladimir V. Balepin Multi-mode multi-propellant liquid rocket engine
US20040103639A1 (en) * 2001-01-11 2004-06-03 Volvo Aero Corporation Rocket engine member and a method for manufacturing a rocket engine member
US20040177603A1 (en) * 2003-03-12 2004-09-16 Aerojet-General Corporation Expander cycle rocket engine with staged combustion and heat exchange

Family Cites Families (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2550277A (en) * 1946-04-05 1951-04-24 Glaces Et Cremes Glacees Ch Ge Cold holdover element
US2701441A (en) * 1950-01-18 1955-02-08 Gen Electric Pressurized feed for jet propulsion systems
US2991617A (en) * 1950-12-01 1961-07-11 Gen Electric Jet motor combustion chamber
US3049870A (en) * 1960-04-14 1962-08-21 United Aircraft Corp Rocket propellant cycle
US3378204A (en) * 1966-01-14 1968-04-16 Thiokol Chemical Corp Nozzle
US3882676A (en) * 1972-11-01 1975-05-13 Messerschmitt Boelkow Blohm Main stream liquid-fuel rocket engine construction
US4073138A (en) * 1974-05-28 1978-02-14 Aerojet-General Corporation Mixed mode rocket engine
US4220001A (en) * 1977-08-17 1980-09-02 Aerojet-General Corporation Dual expander rocket engine
DE2743983C2 (de) * 1977-09-30 1982-11-11 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Flüssigkeitsraketentriebwerk in Nebenstrombauart für den Betrieb im luftleeren Raum
US4589253A (en) * 1984-04-16 1986-05-20 Rockwell International Corporation Pre-regenerated staged-combustion rocket engine
JPS61232371A (ja) 1985-04-05 1986-10-16 Mitsubishi Electric Corp ポンプ式推進装置
US4912925A (en) * 1985-10-04 1990-04-03 United Technologies Corporation Rocket engine with redundant capabilities
US4771599A (en) * 1986-10-20 1988-09-20 United Technologies Corporation Tripropellant rocket engine with injector
US4771600A (en) * 1986-10-20 1988-09-20 United Technologies Corporation Tripropellant rocket engine
JPH0192560A (ja) * 1987-10-02 1989-04-11 Natl Aerospace Lab ロケット噴射器
DE3811613A1 (de) * 1988-04-07 1989-10-19 Messerschmitt Boelkow Blohm Oberflaechenstruktur
GB8811126D0 (en) * 1988-05-11 1988-12-14 Royal Ordnance Plc Bipropellant rocket engines
US4998410A (en) * 1989-09-05 1991-03-12 Rockwell International Corporation Hybrid staged combustion-expander topping cycle engine
US5014507A (en) * 1989-12-14 1991-05-14 Sundstrand Corporation Direct drive gaseous hydrogen turbo actuator
JP2615413B2 (ja) * 1994-02-28 1997-05-28 科学技術庁航空宇宙技術研究所長 複合サイクルロケットエンジン
US5551230A (en) * 1994-03-14 1996-09-03 Rockwell International Corporation Heat induced high pressure lox pump rocket engine cycle
JP3640692B2 (ja) * 1994-11-29 2005-04-20 エア・ウォーター株式会社 船舶推進機関
JP3040695B2 (ja) * 1995-06-09 2000-05-15 三菱重工業株式会社 液体ロケットエンジン
FR2766232B1 (fr) * 1997-07-18 1999-08-20 Snecma Dispositif de refroidissement ou d'echauffement d'un carter circulaire
JP4271866B2 (ja) * 1998-11-27 2009-06-03 ボルボ エアロ コーポレイション 冷却されるノズル壁を有するロケットノズルのノズル構造
JP2000248994A (ja) * 1999-03-01 2000-09-12 Ishikawajima Harima Heavy Ind Co Ltd ロケットエンジンの推薬加圧装置
RU2273756C2 (ru) * 2001-01-11 2006-04-10 Вольво Аэро Корпорейшн Элемент ракетного двигателя и способ изготовления такого элемента ракетного двигателя
JP4019218B2 (ja) * 2001-01-11 2007-12-12 ボルボ エアロ コーポレイション ロケットエンジン部材並びにロケットエンジン部材の製造方法
US6505463B2 (en) * 2001-01-17 2003-01-14 Trw Inc. Pre-burner operating method for rocket turbopump
US7596940B2 (en) * 2005-03-22 2009-10-06 Pratt & Whitney Rocketdyne, Inc. Rocket engine nozzle and method of fabricating a rocket engine nozzle using pressure brazing
US7389636B2 (en) * 2005-07-06 2008-06-24 United Technologies Corporation Booster rocket engine using gaseous hydrocarbon in catalytically enhanced gas generator cycle
US7784269B1 (en) * 2006-08-25 2010-08-31 Xcor Aerospace System and method for cooling rocket engines

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3267664A (en) * 1963-03-19 1966-08-23 North American Aviation Inc Method of and device for cooling
US4879874A (en) * 1986-05-07 1989-11-14 National Space Development Agency Of Japan Liquid fuel rocket engine
US4831818A (en) * 1988-03-09 1989-05-23 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Dual-fuel, dual-mode rocket engine
US6619031B1 (en) * 2000-04-27 2003-09-16 Vladimir V. Balepin Multi-mode multi-propellant liquid rocket engine
US20040103639A1 (en) * 2001-01-11 2004-06-03 Volvo Aero Corporation Rocket engine member and a method for manufacturing a rocket engine member
US20040177603A1 (en) * 2003-03-12 2004-09-16 Aerojet-General Corporation Expander cycle rocket engine with staged combustion and heat exchange

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of WO2008004744A1 *

Also Published As

Publication number Publication date
JP2009540190A (ja) 2009-11-19
WO2008004744A1 (fr) 2008-01-10
EP2038536A1 (fr) 2009-03-25
US20090013663A1 (en) 2009-01-15
JP4824814B2 (ja) 2011-11-30
KR100674118B1 (ko) 2007-01-24

Similar Documents

Publication Publication Date Title
EP2038536A4 (fr) Moteur à méthane pour propulsion de fusée
GB2442337B (en) Turbofan jet engine
GB2473578B (en) Gas turbine engine system
EP2037126A4 (fr) Moteur à double flux
PL1961655T3 (pl) Zespół śruby napędowej do łodzi
EP2116705A4 (fr) Moteur à quatre temps
GB0713072D0 (en) Search engine
EP2235329A4 (fr) Turbine à gaz
GB0616740D0 (en) Aircraft engine thrust reverser
EP2146076A4 (fr) Moteur à quatre temps
ZA200902309B (en) Enclosed shaft system for marine propulsion
EP2148065A4 (fr) Turbine à gaz
PT1902944T (pt) Motor de navio
GB0715667D0 (en) Gas turbine engine
ZA201102888B (en) Thrust engine
GB0600384D0 (en) Cryogenic engines
GB0610592D0 (en) Alternative turbine propulsion
PL380050A1 (pl) Stałe paliwo rakietowe
GB0723731D0 (en) Integral propulsion engine
GB0608796D0 (en) Hybrid engine
GB0617045D0 (en) Aero marine engine (steadfaste)
AU2007904070A0 (en) Multimode jet engine
GB0616556D0 (en) Aviation turbine engine
AU2007901443A0 (en) Water gas engine
PL381470A1 (pl) Silnik żaglowy naddachowy

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20080820

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC MT NL PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA HR MK RS

DAX Request for extension of the european patent (deleted)
RBV Designated contracting states (corrected)

Designated state(s): DE FR IT

RIC1 Information provided on ipc code assigned before grant

Ipc: F02K 9/64 20060101ALI20110329BHEP

Ipc: F02K 9/58 20060101ALI20110329BHEP

Ipc: F02K 9/48 20060101ALI20110329BHEP

Ipc: F02K 9/42 20060101AFI20080311BHEP

A4 Supplementary search report drawn up and despatched

Effective date: 20110408

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION HAS BEEN WITHDRAWN

18W Application withdrawn

Effective date: 20111027